Combustion characteristics and detailed simulations of surrogates for a Tier II gasoline certification fuel

An experimental and numerical study of combustion of a gasoline certification fuel ('indolene'), and four (S4) and fiv e (S5) component surrogates for it, is reported for the configurations of an isolated droplet burning with near spherical symmetry in the standard atmosphere, and a single cylinder engine designed for advanced compression ignition of pre-vaporized fuel. The intent was to compare performance of the surrogate for these different combustion configurations and to assess the broader applicability of the kinetic mechanism and property database for the simulations. A kinetic mechanism comprised of 297 species and 16,797 reactions was used in the simulations that included soot formation and evolution, and accounted for unsteady transport, liquid diffusion inside the droplet, radiative heat transfer, and variable properties. The droplet data showed a clear preference for the S5 surrogate in terms of burning rate. The simulations showed generally very good agreement with measured droplet, flame, and soot shell diameters. Measurements of combustion timing, in-cylinder pressure, and mass-averaged gas temperature were also well predicted with a slight preference for the S5 surrogate. Preferential vaporization was not evidenced from the evolution of droplet diameter but was clearly revealed in simulations of the evolution of mixture fractions inside the droplets. The influence of initial droplet diameter (D o ) on droplet burning was strong, with S5 burning rates decreasing with increasing D o due to increasing radiation losses from the flame. Flame extinction was predicted for D o = 3.0 mm as a radiative loss mechanism but not predicted for smaller D o for the conditions of the simulations.& COPY; 2022 Published by Elsevier Inc. on behalf of The Combustion Institute.

Automated summary

An experimental and numerical study was conducted to investigate the combustion of a gasoline certification fuel and its surrogates in different combustion configurations. The study compared the performance of the surrogates and assessed the applicability of the kinetic mechanism and property database for simulations. The results showed that the S5 surrogate had a higher burning rate and good agreement was observed between the simulations and experimental measurements. The initial droplet diameter significantly influenced the droplet burning, with larger diameters resulting in decreased burning rates due to increased radiation losses.